US5767389A - Method and apparatus for testing a fluid pressure apparatus - Google Patents

Method and apparatus for testing a fluid pressure apparatus Download PDF

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Publication number
US5767389A
US5767389A US08/507,108 US50710895A US5767389A US 5767389 A US5767389 A US 5767389A US 50710895 A US50710895 A US 50710895A US 5767389 A US5767389 A US 5767389A
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United States
Prior art keywords
signature
pressure
chamber
assembly
fill
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Ceased
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US08/507,108
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English (en)
Inventor
Robert Henry LaFountain
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Automotive Products USA Inc
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Automotive Products USA Inc
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Assigned to AUTOMOTIVE PRODUCTS PLC reassignment AUTOMOTIVE PRODUCTS PLC ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: LAFOUNTAIN, ROBERT HENRY
Priority to US08/507,108 priority Critical patent/US5767389A/en
Assigned to AUTOMOTIVE PRODUCTS (USA), INC. reassignment AUTOMOTIVE PRODUCTS (USA), INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: AUTOMOTIVE PRODUCTS PLC
Priority to JP9507396A priority patent/JPH10507512A/ja
Priority to PCT/IB1996/000704 priority patent/WO1997005395A1/en
Priority to KR1019970701986A priority patent/KR970706458A/ko
Priority to EP96921044A priority patent/EP0783633B1/de
Priority to GB9704695A priority patent/GB2307952B/en
Priority to DE69619957T priority patent/DE69619957T2/de
Priority to BR9606539A priority patent/BR9606539A/pt
Publication of US5767389A publication Critical patent/US5767389A/en
Application granted granted Critical
Priority to US09/408,627 priority patent/USRE37151E1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B19/00—Testing; Calibrating; Fault detection or monitoring; Simulation or modelling of fluid-pressure systems or apparatus not otherwise provided for
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M3/00—Investigating fluid-tightness of structures
    • G01M3/02—Investigating fluid-tightness of structures by using fluid or vacuum
    • G01M3/26—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors

Definitions

  • the present invention relates to hydraulic apparatus in general and more particularly to a hydraulic control apparatus comprising a hydraulic master cylinder and a hydraulic slave cylinder for operating a mechanism remotely located from the master cylinder, the hydraulic control apparatus being prefilled with hydraulic fluid and pretested prior to shipment to a motor vehicle manufacturer for installation in a motor vehicle.
  • prefilling with hydraulic fluid and pretesting hydraulic apparatus for operating motor vehicle mechanisms such as mechanical clutches presents the many advantages, for the motor vehicle manufacturer, of receiving a fully assembled mechanism comprising all of the components filled with hydraulic fluid and pretested for proper operation ready to install on a motor vehicle on the assembly line without requiring that the components be installed, separately connected by way of a flexible conduit, and filled after installation with hydraulic fluid while being purged of any atmospheric air contained in the apparatus.
  • liquid is supplied through the open top of the reservoir until the liquid bleeds out of a bleed port in the slave cylinder whereupon the filling is terminated.
  • a port is provided in a side wall of the reservoir, vacuum is applied to the system through the port to evacuate the system, liquid is introduced into the system through the port, and the port is thereafter sealed with a plug which serves to allow flow of hydraulic fluid out of the reservoir upon excess pressure but prevents reverse flow.
  • the apparatus is filled by the use of a filling head which is fitted into the open top of the reservoir and which includes a nozzle portion having an exterior surface enclosing a volume which approximates the volume of the diaphragm so that, following filling of the apparatus, removal of the filling head, and reinsertion of the diaphragm, the apparatus is automatically placed in the totally filled condition.
  • a filling head which is fitted into the open top of the reservoir and which includes a nozzle portion having an exterior surface enclosing a volume which approximates the volume of the diaphragm so that, following filling of the apparatus, removal of the filling head, and reinsertion of the diaphragm, the apparatus is automatically placed in the totally filled condition.
  • the system is closed to substantially preclude escape of hydraulic fluid from the cylinder bore through the conduit means, a predetermined force is applied to the piston to urge the piston to move in the cylinder bore, and the magnitude of the movement of the piston in the cylinder bore in response to the predetermined force is measured to determine the acceptability or unacceptability of the unit under test.
  • This invention is directed to the provision of improved method and apparatus for testing the integrity of a fluid pressure apparatus.
  • this invention is directed to the provision of improved method and apparatus for filling, and testing the integrity of, a fluid pressure apparatus.
  • this invention is directed to the provision of an improved method and apparatus for prefilling a hydraulic control apparatus.
  • the invention methodology relates to the testing and filling of a fluid pressure apparatus having a fluid pressure chamber.
  • the fluid pressure apparatus may comprise a hydraulic control apparatus including a slave cylinder; a conduit connected to one end of the inlet port and the slave cylinder; a master cylinder connected at its discharge port to the other end of the conduit; and a reservoir assembly associated with the master cylinder.
  • the mass of the fluid in the chamber of the fluid pressure apparatus is gradually varied; the pressure in the chamber is noted at successive times as the mass is varied, whereby to generate successive pressure reading; a signature is created from the pressure reading; and the signature is compared to a known stored signature of a satisfactory apparatus.
  • the step of gradually varying the mass of fluid in the chamber comprises evacuating air from the chamber to gradually reduce the pressure in the chamber.
  • This evacuation step which precedes the filling step, is thus utilized to test the integrity of the apparatus.
  • the step of gradually varying the mass of fluid in the chamber comprises gradually filling the chamber with a fluid.
  • the filling step, following the evacuating step is utilized to provide a further determination with respect to the integrity of the apparatus.
  • the step of gradually varying the mass of fluid in the chamber comprises evacuating air from the chamber to gradually reduce the pressure in the chamber, and thereafter filling the chamber with a fluid;
  • the step of noting the pressure in the chamber at successive times comprises noting the pressure in the chamber at successive times as the chamber is evacuated and thereafter noting the pressure in the chamber at successive times as the chamber is filled;
  • the step of creating a signature from the pressure readings comprises creating a vacuum signature as the chamber is evacuated and creating a fill signature as the chamber is thereafter filled;
  • the step of comparing the signature to a known storage signature comprises comparing the vacuum signature to a known stored vacuum signature and thereafter comparing the fill signature to a second known stored fill signature.
  • FIG. 1 is a schematic view of the invention test apparatus
  • FIG. 2 is a perspective somewhat diagrammatic view of the invention test apparatus
  • FIGS. 3 and 4 are vacuum and pressure signatures, respectively, generated by the invention test apparatus.
  • FIG. 5 is a detail view of an encoder utilized in the invention test apparatus.
  • test apparatus 10 is intended for use in filling, and testing the integrity of, a fluid pressure apparatus having a fluid pressure chamber.
  • test apparatus 10 may be utilized to fill and test hydraulic control apparatus or assembly 12.
  • Hydraulic apparatus 12 includes a master cylinder 14 including a housing 16, a reservoir 18, a piston 20, and a push rod 22; a slave cylinder 24 including a housing 26, a piston 28, and a push rod 30; and a conduit 32 interconnecting the discharge end 14a of the master cylinder with the intake end 24a of the slave cylinder.
  • Apparatus 12 may comprise, for example, a clutch control apparatus for a motor vehicle in which the apparatus is supplied to a motor vehicle manufactured in prefilled and pretested form so that the clutch control apparatus is ready for use simply by connecting the push rod 22 to the clutch pedal of the motor vehicle and associating the push rod 30 with a control lever for the clutch throw out bearing.
  • Test apparatus 10 includes a fixture 34, an evacuate/fill conduit 36 including a trap 36a; an evacuation system 38, a fill system 40, a scavenge system 42, and an evaluation system 44.
  • Fixture 34 is configured to hold the housing 16 of master cylinder 14 so as to preclude movement of the master cylinder during the test procedure.
  • Evacuate/fill conduit 36 includes a free or distal end 36b communicating with reservoir 18 and another end 36c.
  • Evacuation system 38 includes a conduit 46, a conduit 48 connecting with conduit 46 and with the other end 36c of conduit 36, a pair of solenoid valves 50 and 52 interposed serially in conduit 46, a vacuum pump 54 communicating with the distal end of conduit 46, and a trap 56 interposed between solenoid valve 52 and vacuum pump 54.
  • Fill system 40 includes an oil cylinder 58 including a piston 60, an air cylinder 62 including a piston 64, a connecting rod 66 connecting pistons 60 and 64, a linear incremental optical encoder 68 including a sensor 70 mounted on connecting rod 66 and a fixed optical bar 71 positioned in a gap 70a of the sensor, a conduit 72 communicating with one end of the oil cylinder, a conduit 74 extending between conduit 72 and one end of conduit 48, a solenoid valve 76 in conduit 74, a check valve 78 in conduit 48, a conduit 79 connecting with the upper end of conduit 72, and a solenoid valve 80 interposed in conduit 79.
  • Scavenge system 42 includes a conduit 81 connected to the other end of conduit 48, a solenoid valve 82 interposed in conduit 81, and a scavenge pump 84 connected to the distal or free end 81a of conduit 81.
  • Evaluation system 44 includes a transducer 86, an A/D converter 87, a clock 88, a signature generator 90, a computer 92, a comparator 94, a printer 96, and leads 98, 100, 102, 104, 106, 108, 110 and 112.
  • Transducer 86 may take any of several well known forms and, for example, may comprise a unit available from DCT Instruments of Columbus, Ohio, as Part No. PTG15VB. Transducer 86 includes a probe 86a communicating with test/fill conduit 36 and operative to sense the pressure in the conduit 36 at all times. Transducer 86 functions in known manner to convert the pressure signal sensed by the probe 86a to an output analog electrical signal on lead 98 having a magnitude proportioned to the magnitude of the sensed pressure signal.
  • A/D convertor 87 receives the analog signal on lead 98 and converts the analog signal in known manner to a corresponding digital signal for further transmission on lead 111.
  • Clock 88 is of known form and functions to emit a clocking or time pulsed signal at selected periodic intervals.
  • Signature generator 90 functions to generate a first signature 114 comprising an evacuation or vacuum signature and a second signature 116 comprising a pressure or fill signature 116.
  • Comparator 94 functions to store signatures corresponding to known satisfactory apparatus 12 and, specifically, stores a first vacuum signature 118 corresponding generally to signature 114 and a second fill signature 120 corresponding generally to fill signature 116. Signatures 118 and 120 are stored in computer 92 by testing a plurality of known satisfactory apparatus 12 to generate satisfactory evacuate and fill signatures.
  • Comparator 94 receives signatures 114/116 from generator 90 on lead 106 and signatures 118/120 from computer 92 on lead 110, compares the respective signatures and make decisions with respect to the acceptability or unacceptability of the apparatus under test based on the extent to which the signatures generated by generator 90 correspond to the stored signatures in computer 92.
  • a light console 122 on comparator 94 includes a yellow light 122a indicating that a test is in progress, a green light 122b indicating that the unit under test is satisfactory, and a red light 122c indicating that the unit under test is unsatisfactory.
  • Printer 96 communicates with comparator 94 via lead 108 and functions, upon a signal from comparator 94, to print a detachable label 124 for securement to the defective apparatus. Specifically, when the comparator 94 determines that an apparatus under test is unsatisfactory it generates a signal via lead 108 for transmission to printer 96 whereupon the printer functions to print out a label 124 for securement to the failed apparatus.
  • the information generated by comparator 94 with respect to each failed unit includes not only the fact that the unit has failed but also the specific nature of the defect causing the failure.
  • Label 124 generated by printer 96 embodies a number or letter code identifying the specific defect of the apparatus.
  • control apparatus or assembly 12 is received at the test apparatus 10 following assembly of the control assembly 12 in known manner on a production line basis.
  • the master cylinder 14 of the assembly is fixedly secured in the fixture 34, the distal end 36b of evacuate/fill conduit 36 is inserted into the reservoir of the master cylinder, and the push rod 30 of the slave cylinder is held in a contracted position by the utilization of, for example, a shipping strap 126.
  • vacuum pump 54 is actuated so as to begin to suck air out of the apparatus 12 via conduits 46, 48 and 36.
  • the pressure in the conduit drops gradually and this pressure is constantly sensed by transducer 86 so that transducer 86 generates a continuous but gradually dropping analog electrical signal on lead 98 for transmittal to A/D convertor 87 where the analog signal on line 98 is converted to a corresponding digital signal whereafter the digital signal is mixed with a clock signal on line 102 and the combined signal is fed to generator 90 to generate vacuum signature 114, best seen in FIG. 3.
  • signature 114 comprises a plot of pressure versus time, begins at approximately atmospheric or 14.7 psi, and gradually drops as air is exhausted from the pressure chambers of the apparatus 12, reaching a final value of approximately 0.002 psi after a time lapse of for example 12 seconds.
  • Critical and telltale points on the signature curve include the shape of the entry knee 114a, the location of the outgassing blip 114b (indicating the release of volatiles or air trapped in pores of the cylinders under test), the slope of the signature line in the region 114c, and the specific location of the diffusion point 114d (the point at which there is no longer enough pressure in the system to push air out).
  • the vacuum signature is transmitted in progress by lead 106 to comparator 94 and the comparable portion of the stored vacuum signal 118 in the computer 92 is gradually and simultaneously transmitted via lead 110 to the comparator 94 so that the instantaneous and progressively developing signature from the assembly under test and the stored signature of a proper assembly are gradually and simultaneously displayed and compared.
  • the instantaneously generated signature and the stored signature may be compared at the end of graph section A after approximately three seconds of test. If the comparison reveals a discrepancy indicative of a defect, the test is immediately aborted and the test assembly is rejected. The operator is apprised of the rejection by illumination of the red light 122c on the light console 122 and the operator is precluded from releasing the master cylinder 14 from the test fixture 34 until he has performed an act, such as pressing a button or moving a lever, to indicate that he has noticed the red light and has therefore noticed that the unit under test is defective.
  • a signal is transmitted from the comparator to the printer, indicating that a defect has been noted and indicating the precise nature of the defect, and the printer 96 thereupon prints a label 124 indicating by letter or by number the nature of the defect, which label may be detached by the operator and positioned on the defective assembly to facilitate repair of the assembly for subsequent retesting.
  • section B If the comparison of sections A of the instantaneous and stored signatures does not reveal a defect, the test is continued and proceeds through section B. At the conclusion of section B, an instantaneous and stored signature are again compared, and a decision is again made with the acceptability or unacceptability of the assembly.
  • This section by section comparison procedure continues until the test has proceeded through all four sections whereupon, assuming that the test assembly has passed at each comparison at the end of each section, the green light 122B is illuminated to apprise the operator that the assembly has passed the vacuum test. At such time as the test assembly is determined to have a defect, the exact nature of the defect may then be ascertained utilizing a lookup table incorporated in the comparator and/or the computer.
  • Defects that may be identified utilizing signature section A include gross part leaks and blocked or skived tubes or connectors.
  • Defects that may be identified utilizing signature section B include reversed seals in the master cylinder, damaged seals in the master cylinder, missing or wrong components in the master cylinder, defective or damaged pistons in the master cylinder, center feed problems, blocked or skived tubes, fine leaks in the master cylinder, or scratched bores in the master or slave cylinder.
  • Defects that may be identified utilizing signature section C include fine leaks in the slave cylinder and damaged connector seals.
  • Defects that may be identified utilizing signature section D include unknown abnormalities or anomalies and out of tolerance parts.
  • valves 50 and 52 are closed, valve 76 is opened, and air under pressure is delivered to air cylinder 62 via conduit 128 to move the piston 64 forwardly and thereby move the piston 60 of the oil cylinder forwardly to eject hydraulic fluid out of the oil cylinder.
  • the oil leaving the oil cylinder flows through conduit 72, conduit 74, valve 76, conduit 48, and check valve 78 to conduit 36 and thereafter into the reservoir 18 to begin filling the pressure chambers of the assembly under test.
  • transducer 86 continues to sense the pressure in the conduit 36 and continues to generate an analog signal on lead 98 for transmittal to A/D convertor 87 and transmittal via lead 111 and 104 to generator 90.
  • This signal is mixed with a digital signal on lead 112 from encoder 68 generated by movement of the sensor 70 with connecting rod 66 relative to fixed optical bar 71 as pistons 60 and 54 continue to move forwardly.
  • optical bar 71 includes a plurality of equally, linearly spaced slits 71a; sensor 70 includes a diode 70b and a light detector 70c positioned on opposite sides of gap 70a; and the digital signal on lead 112 from encoder 68 is generated every time a beam is completed across the gap 70a between diode 70b and detector 70c by virtue of alignment of the diode and detector with a slit 71a.
  • the fill signature developed during the fill cycle is seen in FIG. 4 and comprises a plot of pressure versus pulses of the encoder, which are indicative of the position of piston 60 of fill cylinder 58.
  • the analog signal generated by transducer 86 is read periodically in response to triggering from the encoder 68.
  • encoder 68 triggers A/D converter 87 to take a reading from transducer 86 every time the encoder ends a unit of movement as sensed by the alignment of the diode/detector 70b, 70c of the sensor with a slit 71a in the optical bar.
  • the plot seen in FIG. 4 therefore includes a plurality of points generated at the end of each unit of linear movement of the connecting rod 66 as determined by the movement of sensor 70 with respect to bar 71.
  • the pressure sensed by the transducer 86 during the course of the fill cycle ranges from essentially zero pressure during the initial portion of the cycle to approximately 35 psi at the maximum pressure in the cycle.
  • Notable and significant points on the fill signature 116 include a flat introductory portion 116a indicating the filling of the conduits leading to the assembly under test; a blip 116b indicating filling of the reservoir of the master cylinder; a steep slope portion 116c indicating movement of the oil through the orifice extending between the reservoir and the bore of the master cylinder; a blip 116d indicating the start of the filling of the master cylinder; a dwell portion 116e indicating continued filling of the master cylinder; a blip 116f indicating the beginning of the filling of the conduit 32; a steep slope portion 116g indicating the continued filling of the conduit; a blip 116h indicating the start of the filling of the slave cylinder; a plateau portion 116i indicating continued filling of the slave cylinder; and a blip 116j indicating the end of the fill cycle, whereafter the pressure falls off sharply and returns essentially to atmospheric.
  • comparison of the stored fill signature 120 to the instantaneously generated fill signature 116 may be delayed until the fill cycle has been completed but, preferably, comparisons are made at the end of each of a plurality of signature sections A, B and C and the test is aborted at such time as any one of these comparisons indicates a defect.
  • the comparator sends a signal to the printer 96 (to print a label 124 bearing a letter or number identifying the nature of the defect for attachment to the defective assembly under test) and causes the illumination of red light 122C (to apprise the operator that the assembly under test has failed and require the operator to perform a predetermined manual acknowledging operation prior to release of the assembly under test by fixture 34).
  • Defects that may be identified utilizing fill signature section A include system integrity, improper reservoir, improper supply hose, reversed or damaged master cylinder seals, center feed problems, missing or improper master cylinder components, and blocked or skived tubes or master cylinder end connectors.
  • Defects that may be identified utilizing fill signature Section B include improper conduit between master cylinder and slave cylinder, blocked or skived conduits or slave cylinder end connector, and improper connectors.
  • Defects that may be identified utilizing fill signature section C include improper slave cylinder, reverse seal in the slave cylinder, damaged or defective seal in the slave cylinder, damaged or defective piston in the slave cylinder, and missing or improper components.
  • valve 76 is closed, valves 80 and 82 are opened, scavenge pump 84 is actuated, and the pressurized air supply to air cylinder 62 via conduits 128 is reversed. Reversing of the pressurized air supply to air cylinder 62 causes piston 60 to retreat in air cylinder 58; opening of valve 80 allows make-up oil to flow through conduit 79 and 72 to fill in the oil cylinder behind the retreating piston; and the actuation of the scavenge pump in conjunction with the opening of valve 82 allows the scavenge pump to suck residual oil in the system out of the system in preparation for the next test cycle.
  • the test is immediately terminated.
  • the operator is apprised of the failure by virtue of illumination of the red light 122c, and the operator, after acknowledging recognition of the failure by a suitable manual act, releases the master cylinder from the fixture 34 and places the failed apparatus 12 on a conveyor line leading to a rebuild station.
  • the operator notes the label on the failed unit and specifically notes the specific letter or number code on the label indicating the specific defect in the unit, whereby to aid the repair person in the repair procedure.
  • the unit is placed again on the main conveyor line leading to the test/fill station where the unit is again tested and filled, and hopefully, passed on for shipment.
  • the initial vacuum test detect the vast majority of the defective units while the units are still in a dry and therefore reusable condition
  • the subsequent pressure test detect those few defective units that were not detected by the vacuum test so that only a small percentage of the defective units that are ultimately detected comprise wet units that must be discarded.
  • the test is quicker and, in fact, reduces the total evacuate and fill time by approximately 50%; the apparatus required to perform the testing is smaller and therefore takes up less space on the floor of the manufacturing and testing facilities; the test is more accurate since it involves a double test wherein the vast majority of the defective units are detected in the vacuum test and the remaining defective units are detected in the following fill test; since the vast majority of the defective units are detected in the vacuum test before they have been filled, only a few of the defective units are detected after filling and therefore only a few of the defective units have to be discarded; the system can be used to find and eliminate problems in the overall procedure rather than to simply detect bad units and as such provides a means of refining and improving the assembly process rather than simply a means of eliminating bad units resulting from the assembly process; and the fixturing required to hold the units under test is greatly improved and specifically is smaller, simpler, lends itself to modular
  • the method of the invention may also be applied to systems (such as clutch or brake systems) that have already been incorporated into a motor vehicle in a dry condition as part of the overall motor vehicle assembly process in which case the invention method is used to test and fill the dry units in situ on the vehicle.
  • systems such as clutch or brake systems
  • the present invention is applicable to the testing and filling of any fluid pressure apparatus having a fluid pressure chamber.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Examining Or Testing Airtightness (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Measuring Fluid Pressure (AREA)
  • Hydraulic Clutches, Magnetic Clutches, Fluid Clutches, And Fluid Joints (AREA)
US08/507,108 1995-07-26 1995-07-26 Method and apparatus for testing a fluid pressure apparatus Ceased US5767389A (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
US08/507,108 US5767389A (en) 1995-07-26 1995-07-26 Method and apparatus for testing a fluid pressure apparatus
BR9606539A BR9606539A (pt) 1995-07-26 1996-07-16 Processo de teste e aparelho para enchimento e teste da integridade de conjunto de pressao fluída
JP9507396A JPH10507512A (ja) 1995-07-26 1996-07-16 流体圧装置のテスト方法及び装置
PCT/IB1996/000704 WO1997005395A1 (en) 1995-07-26 1996-07-16 Method and apparatus for testing a fluid pressure apparatus
KR1019970701986A KR970706458A (ko) 1995-07-26 1996-07-16 유체압력장치의 시험방법과 장치(method and apparatus for testing a fluid pressoure apparatus)
EP96921044A EP0783633B1 (de) 1995-07-26 1996-07-16 Verfahren und vorrichtung zum testen von eine hydraulische vorrichtung
GB9704695A GB2307952B (en) 1995-07-26 1996-07-16 Method and apparatus for testing a fluid pressure apparatus
DE69619957T DE69619957T2 (de) 1995-07-26 1996-07-16 Verfahren und vorrichtung zum testen von eine hydraulische vorrichtung
US09/408,627 USRE37151E1 (en) 1995-07-26 1999-09-30 Method and apparatus for testing a fluid pressure apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/507,108 US5767389A (en) 1995-07-26 1995-07-26 Method and apparatus for testing a fluid pressure apparatus

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US09/408,627 Reissue USRE37151E1 (en) 1995-07-26 1999-09-30 Method and apparatus for testing a fluid pressure apparatus

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US5767389A true US5767389A (en) 1998-06-16

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US08/507,108 Ceased US5767389A (en) 1995-07-26 1995-07-26 Method and apparatus for testing a fluid pressure apparatus
US09/408,627 Expired - Fee Related USRE37151E1 (en) 1995-07-26 1999-09-30 Method and apparatus for testing a fluid pressure apparatus

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US09/408,627 Expired - Fee Related USRE37151E1 (en) 1995-07-26 1999-09-30 Method and apparatus for testing a fluid pressure apparatus

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US (2) US5767389A (de)
EP (1) EP0783633B1 (de)
JP (1) JPH10507512A (de)
KR (1) KR970706458A (de)
BR (1) BR9606539A (de)
DE (1) DE69619957T2 (de)
GB (1) GB2307952B (de)
WO (1) WO1997005395A1 (de)

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US6081767A (en) * 1996-09-13 2000-06-27 Sun Electric Systems B.V. Method and device for determining the amount of undissolved gas in a hydraulic system
US6374663B1 (en) * 1997-04-30 2002-04-23 Volvo Personvagnar Ab Method and device for leakage testing in a tank system
EP1577657A2 (de) * 2004-03-18 2005-09-21 Friedrich Boysen GmbH & Co. KG Verfahren und Vorrichtung zur Dichtheitsprüfung einer Abgasanlage
KR100783621B1 (ko) 2006-03-28 2007-12-07 한국에너지기술연구원 리니어엔진의 유압식 동력측정장치 및 이에 따른 작동방법
US7614283B2 (en) 2006-04-17 2009-11-10 Lincoln Industrial Corporation Cooling system testing apparatus and methods
US8196615B1 (en) 2008-04-21 2012-06-12 Jim Browarny Liquid/air pressure testing tool
DE102011075168A1 (de) * 2011-05-03 2012-11-08 Zf Friedrichshafen Ag Verfahren zum Erkennen und Berücksichtigen einer Leckage in der Stellvorrichtung einer druckmittelbetätigten Kupplung
KR101492250B1 (ko) * 2014-06-10 2015-02-13 디와이파워 주식회사 유압 실린더의 내부 누유량 측정 장치
CN108506279A (zh) * 2018-03-26 2018-09-07 华中科技大学 一种高压气动伺服阀质量流量特性测定装置及方法
US10656038B2 (en) * 2018-07-30 2020-05-19 Honda Motor Co., Ltd. Apparatus, system, and method for use in fluid filling apparatus inspection
CN111929011A (zh) * 2020-08-19 2020-11-13 无锡市新莱珂机械有限公司 一种气密封测试仪及其过滤进气机构和管件检测夹装机构
US11085349B2 (en) 2016-10-07 2021-08-10 Vitesco Technologies GmbH Monitoring a pressure sensor in a hydraulic system of a motor vehicle
US11959521B1 (en) * 2023-06-21 2024-04-16 John R. Mickowski Clutch actuating device

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19628221C2 (de) * 1996-07-15 2000-05-31 Festo Ag & Co Verfahren und Vorrichtung zur Bestimmung von Betriebspositionen einer Arbeitseinrichtung
AU2002365597A1 (en) * 2001-11-09 2003-06-10 Barry John Mason Apparatus for use with a pool cleaner
JP4096599B2 (ja) * 2002-04-10 2008-06-04 株式会社アドヴィックス 液圧制御装置の液圧測定方法、及び液圧制御装置の健全性評価方法
US7231317B2 (en) 2003-01-08 2007-06-12 International Business Machines Corporation Correlating power signatures with automated equipment
DE10355250B4 (de) * 2003-11-26 2005-09-01 Festo Ag & Co. Verfahren und Vorrichtung zur Leckage-Ermittlung
JP5138333B2 (ja) * 2007-10-09 2013-02-06 トヨタ自動車東日本株式会社 ブレーキ検査用圧力装置
KR100941373B1 (ko) * 2009-09-11 2010-02-05 티엠디이엔지(주) 발전 설비용 유압식 액츄에이터 및 그 정비방법
EP2302270B1 (de) * 2009-09-29 2012-09-12 Sun Test Systems B.V. Verfahren zur Bestimmung einer Funktion eines Gasablassventils
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DE102016112971A1 (de) 2016-07-14 2018-01-18 Ipgate Ag Diagnoseverfahren für mindestens eine Komponente eines Kraftfahrzeugs
JP6673141B2 (ja) * 2016-10-20 2020-03-25 トヨタ自動車株式会社 液圧装置の試験方法
DE102017123923B4 (de) * 2017-10-13 2023-05-17 Schunk Gmbh & Co. Kg Spann- Und Greiftechnik Verfahren zur Bestimmung des Drucks in Greifvorrichtungen und/oder von Leckagen und Greifvorrichtung
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US6374663B1 (en) * 1997-04-30 2002-04-23 Volvo Personvagnar Ab Method and device for leakage testing in a tank system
EP1577657A2 (de) * 2004-03-18 2005-09-21 Friedrich Boysen GmbH & Co. KG Verfahren und Vorrichtung zur Dichtheitsprüfung einer Abgasanlage
EP1577657A3 (de) * 2004-03-18 2006-02-15 Friedrich Boysen GmbH & Co. KG Verfahren und Vorrichtung zur Dichtheitsprüfung einer Abgasanlage
KR100783621B1 (ko) 2006-03-28 2007-12-07 한국에너지기술연구원 리니어엔진의 유압식 동력측정장치 및 이에 따른 작동방법
US7614283B2 (en) 2006-04-17 2009-11-10 Lincoln Industrial Corporation Cooling system testing apparatus and methods
US8196615B1 (en) 2008-04-21 2012-06-12 Jim Browarny Liquid/air pressure testing tool
DE102011075168B4 (de) 2011-05-03 2022-02-17 Zf Friedrichshafen Ag Verfahren zum Erkennen und Berücksichtigen einer Leckage in der Stellvorrichtung einer druckmittelbetätigten Kupplung
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CN105298820A (zh) * 2014-06-10 2016-02-03 Dypower株式会社 用于测量从液压缸固有地泄漏的油的设备
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CN108506279A (zh) * 2018-03-26 2018-09-07 华中科技大学 一种高压气动伺服阀质量流量特性测定装置及方法
CN108506279B (zh) * 2018-03-26 2019-06-18 华中科技大学 一种高压气动伺服阀质量流量特性测定装置及方法
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EP0783633B1 (de) 2002-03-20
DE69619957T2 (de) 2003-07-24
DE69619957D1 (de) 2002-04-25
BR9606539A (pt) 1998-06-23
KR970706458A (ko) 1997-11-03
JPH10507512A (ja) 1998-07-21
WO1997005395A1 (en) 1997-02-13
EP0783633A1 (de) 1997-07-16
USRE37151E1 (en) 2001-05-01
GB2307952A (en) 1997-06-11
GB9704695D0 (en) 1997-04-23

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